As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
***CORROSION*** AROUND MAJORITY OF FASTENERS THROUGH FUSELAGE SKIN EXTERNALLY; COVERED BY DORSAL FIN FROM STA 867 TO STA 1006; APPROXIMATELY STR 2R TO STR 2L. / REPAIRED FUSELAGE SKIN B.S 867-1006 STR 2R-2L IAW EA 1-753-36041 REV IR AND ATS ER 19-05567 REV IR